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WO2014081577A1 - Exhaust-gas turbocharger - Google Patents

Exhaust-gas turbocharger Download PDF

Info

Publication number
WO2014081577A1
WO2014081577A1 PCT/US2013/068899 US2013068899W WO2014081577A1 WO 2014081577 A1 WO2014081577 A1 WO 2014081577A1 US 2013068899 W US2013068899 W US 2013068899W WO 2014081577 A1 WO2014081577 A1 WO 2014081577A1
Authority
WO
WIPO (PCT)
Prior art keywords
vane
bearing
exhaust
gas turbocharger
shafts
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US2013/068899
Other languages
French (fr)
Inventor
Jaroslaw Kierat
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BorgWarner Inc
Original Assignee
BorgWarner Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BorgWarner Inc filed Critical BorgWarner Inc
Priority to KR1020157015042A priority Critical patent/KR102074409B1/en
Priority to CN201380058151.6A priority patent/CN104769251B/en
Priority to JP2015542705A priority patent/JP6283682B2/en
Priority to US14/440,979 priority patent/US9745861B2/en
Priority to DE112013005105.2T priority patent/DE112013005105T5/en
Publication of WO2014081577A1 publication Critical patent/WO2014081577A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/165—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for radial flow, i.e. the vanes turning around axes which are essentially parallel to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
    • F02B37/12—Control of the pumps
    • F02B37/24—Control of the pumps by using pumps or turbines with adjustable guide vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
    • F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/40—Application in turbochargers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Definitions

  • the invention relates to an exhaust-gas turbocharger according to the preamble of claim 1.
  • VGT variable turbine geometry
  • a adjusting ring in which guide vanes are adjusted by means of an adjusting ring.
  • the radial bearing of the adjusting ring also has an influence on this, for example.
  • Claims 5 and 6 define a VTG cartridge according to the invention as an object which can be marketed independently.
  • FIG. 1 shows a schematically greatly simplified illustration of an exhaust-gas turbocharger according to the invention
  • Figure 2 shows a sectional illustration of a part of the cartridge, sectioned along the center line of said cartridge,
  • Figure 3 shows a plan view of a part of the VTG cartridge as per Figure 2
  • Figure 4 shows an illustration, corresponding to Figure 2, of a second embodiment
  • Figure 5 shows an illustration, corresponding to Figure 3, of the embodiment as per Figure 4.
  • FIG 1 shows a schematically greatly simplified basic illustration of an exhaust-gas turbocharger 1 according to the invention, which has a charger axis of rotation L.
  • the exhaust-gas turbocharger 1 also has a turbine 2, which comprises a turbine wheel 3 surrounded by an inflow duct 4 which is provided with a so-called VTG cartridge 5.
  • This VTG cartridge 5 will be described in detail hereinbelow with reference to Figures 2 to 4.
  • the exhaust-gas turbocharger 1 also of course has all the other common parts of an exhaust-gas turbocharger, such as a shaft 14, which is mounted rotatably in a bearing housing 15 and which bears the turbine wheel 3 at one end and a compressor wheel 17 of a compressor 16 at the other end. These parts are likewise shown only in schematically greatly simplified form in Figure 1 , since they are not of importance for explaining the principles of the present invention.
  • VTG cartridge which, as mentioned, will be explained in detail hereinbelow with reference to Figures 2 to 5, is likewise shown in greatly schematically simplified form.
  • a VTG cartridge is understood to mean a structural unit which, between a vane bearing ring 7 and a disk (not illustrated), delimits the inflow duct 4 for the passage of exhaust gases to the turbine wheel 3.
  • a VTG cartridge of said type also has a multiplicity of vanes 6 which are arranged in the inflow duct 4.
  • the vanes 6 can be moved rotatably in a vane bearing ring 7 between a closed and an open position.
  • the vanes have vane shafts 9 each having an axis of rotation.
  • the vane shafts 9 in turn are connected to vane levers 10, of which in each case one vane lever is denoted in Figures 2 to 6 with the reference numeral 10.
  • vane levers which are each formed identically and are preferably offset to be provided.
  • Each vane lever 10 has a lever head 11, which engages into an associated groove 12 in an adjusting ring 13.
  • Figure 2 shows that the adjusting ring 13 surrounds the vane bearing ring 7 at the outside, that is to say along the outer circumference of the latter, whereas in Figure 5, said adjusting ring is arranged, in a second possible embodiment, within the vane bearing ring 7.
  • a bearing which, according to the invention, is formed by at least one rolling element 8 which is arranged on a vane shaft 9 of the cartridge 5.
  • a bearing which, according to the invention, is formed by at least one rolling element 8 which is arranged on a vane shaft 9 of the cartridge 5.
  • the bearing elements 8 are preferably formed as bearing sleeves of simple construction.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supercharger (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • General Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Control Of Turbines (AREA)

Abstract

The invention relates to an exhaust-gas turbocharger (1) having a turbine (2) which has a turbine wheel (3) surrounded by an inflow duct (4), and having a VTG cartridge (5), which VTG cartridge has a disk and a vane bearing ring (7) which delimit the inflow duct, and which VTG cartridge has a multiplicity of vanes (6) which are arranged in the inflow duct (4) and which are mounted in the vane bearing ring (7) by way of rotatable vane shafts (9), which vane shafts are connected to vane levers (10), the lever heads (11) of which engage into associated grooves (12) in an adjusting ring (13), wherein the adjusting ring (13) is guided by means of at least one bearing (8) which is arranged on one of the vane shafts (9).

Description

EXHAUST-GAS TURBOCHARGER
DESCRIPTION
The invention relates to an exhaust-gas turbocharger according to the preamble of claim 1.
In the case of such an exhaust-gas turbocharger, provision is made of a variable turbine geometry (VTG), in which guide vanes are adjusted by means of an adjusting ring. In order to be able to provide the best possible control, the least possible hysteresis and thus the least possible friction of the system is desirable. The radial bearing of the adjusting ring also has an influence on this, for example.
In view of this, it is an object of the present invention to provide an exhaust-gas turbocharger of the type indicated in the preamble of claim 1, the structure of which has a simpler and thus more cost-effective design.
This object is achieved by the features of claim 1.
The dependent claims contain advantageous developments of the invention. According to the invention, for mounting purposes, it is possible for rolling bodies, bearing sleeves or the like to be fitted on at least one of the vane shafts and utilized for the mounting of the adjusting ring. In principle, it is also possible for such bearing elements to be provided on all of the vane shafts or only on certain selected vane shafts.
Claims 5 and 6 define a VTG cartridge according to the invention as an object which can be marketed independently.
Further details, features and advantages of the invention become apparent from the following description of exemplary embodiments with reference to the drawing, in which:
Figure 1 shows a schematically greatly simplified illustration of an exhaust-gas turbocharger according to the invention,
Figure 2 shows a sectional illustration of a part of the cartridge, sectioned along the center line of said cartridge,
Figure 3 shows a plan view of a part of the VTG cartridge as per Figure 2, Figure 4 shows an illustration, corresponding to Figure 2, of a second embodiment, and
Figure 5 shows an illustration, corresponding to Figure 3, of the embodiment as per Figure 4.
Figure 1 shows a schematically greatly simplified basic illustration of an exhaust-gas turbocharger 1 according to the invention, which has a charger axis of rotation L. The exhaust-gas turbocharger 1 also has a turbine 2, which comprises a turbine wheel 3 surrounded by an inflow duct 4 which is provided with a so-called VTG cartridge 5. This VTG cartridge 5 will be described in detail hereinbelow with reference to Figures 2 to 4.
The exhaust-gas turbocharger 1 also of course has all the other common parts of an exhaust-gas turbocharger, such as a shaft 14, which is mounted rotatably in a bearing housing 15 and which bears the turbine wheel 3 at one end and a compressor wheel 17 of a compressor 16 at the other end. These parts are likewise shown only in schematically greatly simplified form in Figure 1 , since they are not of importance for explaining the principles of the present invention.
The VTG cartridge, which, as mentioned, will be explained in detail hereinbelow with reference to Figures 2 to 5, is likewise shown in greatly schematically simplified form.
A VTG cartridge is understood to mean a structural unit which, between a vane bearing ring 7 and a disk (not illustrated), delimits the inflow duct 4 for the passage of exhaust gases to the turbine wheel 3. A VTG cartridge of said type also has a multiplicity of vanes 6 which are arranged in the inflow duct 4. The vanes 6 can be moved rotatably in a vane bearing ring 7 between a closed and an open position. For this purpose, the vanes have vane shafts 9 each having an axis of rotation. The vane shafts 9 in turn are connected to vane levers 10, of which in each case one vane lever is denoted in Figures 2 to 6 with the reference numeral 10. In the case of a VTG cartridge 5, it is possible, for example, for ten such vane levers which are each formed identically and are preferably offset to be provided.
Each vane lever 10 has a lever head 11, which engages into an associated groove 12 in an adjusting ring 13. Here, Figure 2 shows that the adjusting ring 13 surrounds the vane bearing ring 7 at the outside, that is to say along the outer circumference of the latter, whereas in Figure 5, said adjusting ring is arranged, in a second possible embodiment, within the vane bearing ring 7.
For the mounting of the adjusting ring 13, provision is made of a bearing which, according to the invention, is formed by at least one rolling element 8 which is arranged on a vane shaft 9 of the cartridge 5. As explained in the introduction, it is also possible for all of the vane shafts 9 to be provided with such bearing elements, or for only a selected subset of the vane shafts 9 to be provided with the bearing elements 8.
The bearing elements 8 are preferably formed as bearing sleeves of simple construction. In addition to the above written disclosure, reference is hereby explicitly made to the illustrative representation of the invention in Figures 1 to 5 to supplement the disclosure of the invention.
List of reference signs
1 Exhaust-gas turbocharger
2 Turbine
3 Turbine wheel
4 Inflow duct
5 VTG cartridge
6 Vane
7 Vane bearing ring
8 Bearing/bearing sleeve
9 Vane shaft
10 Vane lever
1 1 Lever heads
12 Groove
13 Adjusting ring
14 Shaft
15 Bearing housing
16 Compressor
17 Compressor wheel
L Charger longitudinal axis
M Central axis of the cartridge

Claims

1. An exhaust-gas turbocharger ( 1 )
having a turbine (2)
· which has a turbine wheel (3) surrounded by an inflow duct (4), and having a VTG cartridge (5),
• which VTG cartridge has a disk and a vane bearing ring (7) which delimit the inflow duct, and
• which VTG cartridge has a multiplicity of vanes (6) which are arranged in the inflow duct (4) and which are mounted in the vane bearing ring (7) by way of rotatable vane shafts (9), which vane shafts are connected to vane levers (10), the lever heads (11) of which engage into associated grooves (12) in an adjusting ring (13), characterized in that
- the adjusting ring (13) is guided by means of at least one bearing (8) which is arranged on one of the vane shafts (9).
2. The exhaust-gas turbocharger as claimed in claim 1, characterized in that the bearing is in the form of a bearing sleeve.
3. The exhaust-gas turbocharger as claimed in claim 1 or 2, characterized in that a bearing (8) is arranged on each of the vane shafts (9) or on a selectable subset of the vane shafts (9).
4. The exhaust-gas turbocharger as claimed in one of claims 1 to 3, characterized in that the adjusting ring (13) surrounds the vane bearing ring (7) at the outside or is arranged within the vane bearing ring (7).
5. A VTG cartridge (5) of an exhaust-gas turbocharger (1),
having a disk and a vane bearing ring (7) which delimit an inflow duct (4),
- having a multiplicity of vanes which are arranged in the inflow duct (4) and which are mounted in the vane bearing ring (7) by way of rotatable vane shafts (9), which vane shafts are connected to vane levers (10), the lever heads (11) of which engage into associated grooves (12) in an adjusting ring (13),
characterized in that
- the adjusting ring (13) is guided by means of at least one bearing (8) which is arranged on one of the vane shafts (9). The VTG cartridge as claimed in claim 5, characterized by one of claims
PCT/US2013/068899 2012-11-20 2013-11-07 Exhaust-gas turbocharger Ceased WO2014081577A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
KR1020157015042A KR102074409B1 (en) 2012-11-20 2013-11-07 Exhaust-gas turbocharger
CN201380058151.6A CN104769251B (en) 2012-11-20 2013-11-07 Exhaust turbine supercharger
JP2015542705A JP6283682B2 (en) 2012-11-20 2013-11-07 Exhaust gas turbocharger
US14/440,979 US9745861B2 (en) 2012-11-20 2013-11-07 Exhaust-gas turbocharger
DE112013005105.2T DE112013005105T5 (en) 2012-11-20 2013-11-07 turbocharger

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102012022658 2012-11-20
DE102012022658.6 2012-11-20

Publications (1)

Publication Number Publication Date
WO2014081577A1 true WO2014081577A1 (en) 2014-05-30

Family

ID=50776464

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2013/068899 Ceased WO2014081577A1 (en) 2012-11-20 2013-11-07 Exhaust-gas turbocharger

Country Status (6)

Country Link
US (1) US9745861B2 (en)
JP (1) JP6283682B2 (en)
KR (1) KR102074409B1 (en)
CN (1) CN104769251B (en)
DE (1) DE112013005105T5 (en)
WO (1) WO2014081577A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2960151A1 (en) * 2014-06-16 2015-12-30 Rolls-Royce plc A unison ring assembly
US9890656B2 (en) 2014-05-28 2018-02-13 Rolls-Royce Deutschland Ltd & Co Kg Variable stator vane arrangement

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017118794B4 (en) * 2017-08-17 2025-01-02 Ihi Charging Systems International Gmbh Adjustable guide device for a turbine, turbine for an exhaust gas turbocharger and exhaust gas turbocharger

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020168262A1 (en) * 2000-05-19 2002-11-14 Yasuaki Jinnai Nozzle adjustment mechanism for variable-capacity turbine
JP2004138006A (en) * 2002-10-18 2004-05-13 Mitsubishi Heavy Ind Ltd Surface treatment structure and surface treatment method for variable capacity type supercharger
US20070068155A1 (en) * 2005-08-25 2007-03-29 Noriyuki Hayashi Variable-throat exhaust tuebocharger and method for manufacturing constituent members of variable throat mechanism
US20100124489A1 (en) * 2007-12-21 2010-05-20 Hiroshi Suzuki Variable-capacity exhaust turbocharger equipped with variable-nozzle mechanism
US20100150701A1 (en) * 2007-06-26 2010-06-17 Borgwarner Inc. Variable geometry turbocharger

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH11236818A (en) * 1998-02-20 1999-08-31 Taiho Kogyo Co Ltd Turbocharger variable nozzle
US9017017B2 (en) * 2009-04-10 2015-04-28 Honeywell Internatonal Inc. Variable-vane assembly having fixed guide pins for unison ring

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020168262A1 (en) * 2000-05-19 2002-11-14 Yasuaki Jinnai Nozzle adjustment mechanism for variable-capacity turbine
JP2004138006A (en) * 2002-10-18 2004-05-13 Mitsubishi Heavy Ind Ltd Surface treatment structure and surface treatment method for variable capacity type supercharger
US20070068155A1 (en) * 2005-08-25 2007-03-29 Noriyuki Hayashi Variable-throat exhaust tuebocharger and method for manufacturing constituent members of variable throat mechanism
US20100150701A1 (en) * 2007-06-26 2010-06-17 Borgwarner Inc. Variable geometry turbocharger
US20100124489A1 (en) * 2007-12-21 2010-05-20 Hiroshi Suzuki Variable-capacity exhaust turbocharger equipped with variable-nozzle mechanism

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9890656B2 (en) 2014-05-28 2018-02-13 Rolls-Royce Deutschland Ltd & Co Kg Variable stator vane arrangement
EP2960151A1 (en) * 2014-06-16 2015-12-30 Rolls-Royce plc A unison ring assembly

Also Published As

Publication number Publication date
DE112013005105T5 (en) 2015-07-09
CN104769251A (en) 2015-07-08
KR102074409B1 (en) 2020-02-06
JP6283682B2 (en) 2018-02-21
JP2015535055A (en) 2015-12-07
US20150300246A1 (en) 2015-10-22
KR20150084903A (en) 2015-07-22
US9745861B2 (en) 2017-08-29
CN104769251B (en) 2018-09-04

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